Related Books

Wind-tunnel Investigation at High Subsonic Speed of the Static Longitudinal Stability Characteristics of a Winged Reentry Vehicle Having a Large Negatively Deflected Flap-type Control Surface
Language: en
Pages: 24

Wind-tunnel Investigation at High Subsonic Speed of the Static Longitudinal Stability Characteristics of a Winged Reentry Vehicle Having a Large Negatively Deflected Flap-type Control Surface

Authors: Paul G. Fournier
Categories: Aerodynamics
Type: BOOK - Published: 1959 - Publisher:

DOWNLOAD EBOOK

An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels
Language: en
Pages: 40

An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels

Authors: Bernard Spencer
Categories: Aerodynamics
Type: BOOK - Published: 1961 - Publisher:

DOWNLOAD EBOOK

Subsonic aerodynamic characteristics of delta-wing reentry vehicle with vertically displaced and cambered wing-tip panels.
AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4 DEG TO 100 DEG OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS
Language: en
Pages: 32

AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4 DEG TO 100 DEG OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS

Authors: Bernard Spencer
Categories: Air flow
Type: BOOK - Published: 1960 - Publisher:

DOWNLOAD EBOOK

An Investigation at Subsonic Speeds of Aerodynamic Charactersitcs at Angles of Attack from -40 to 1000 of a Delta-wing Reentry Configuration Having Folding Wingtip Panels
Language: en
Pages: 34

An Investigation at Subsonic Speeds of Aerodynamic Charactersitcs at Angles of Attack from -40 to 1000 of a Delta-wing Reentry Configuration Having Folding Wingtip Panels

Authors: Bernard Spencer
Categories: Air flow
Type: BOOK - Published: 1960 - Publisher:

DOWNLOAD EBOOK

Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack Up to 90°
Language: en
Pages: 44

Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack Up to 90°

Authors: John E. Grimaud
Categories: Aerodynamic measurements
Type: BOOK - Published: 1961 - Publisher:

DOWNLOAD EBOOK